Piper Lance II User Manual

LUBRICATING
OIL,
GENERAL
PURPOSE,
LOW
TEMPERATURE
LUBRICATING
OIL,
AIRCRAFT
RECIPRO-
CATING
ENGINE
(PISTON)
GRADE
AS
SPECIFIED
SAE
50
ABOVE
60
F
AIR
TEMP.
SAE
40
30
TO
90°
F AIR
TEMP.
SAE
30
0
°
TO
70°F
AIR
TEMP.
SAE
20
BELOW
10°F
AIR
TEMP.
HYDRAULIC
FLUID
PETROLEUM
BASE
GREASE,
AIRCRAFT
AND
INSTRUMENT,
GEAR
AND
ACTUATOR
SCREW
GREASE,
AIRCRAFT
HIGH
TEMPERATURE
LANCE
II
SERVICE
MANUAL
TYPE
OF
LUBRICANTS
LUBRICANT
SPECIFICATION
PREFERRED
PRODUCT
AND
VENDOR
MIL-L-7870
MIL-L-6082
MIL-H-5606
MIL-G-23827
TEXACO
MARFAK
ALL
PURPOSE
GREASE,
MOBIL
GREASE
77
(OR
MOBILUX
EP2)
SHELL
ALVANIA
EP
GREASE
2
PARKER
O-RING
LUBRICANT
AERO
LUBRIPLATE
FISKE
BROS.
REFINING
CO.
FLUOROCARBON
RELEASE
AGENT
DRY
LUBRICANT
GREASE
-
LUBRICATION
GENERAL
PURPOSE
AIRCRAFT
SILICONE,
COMPOUND
GREASE,
WIDE
TEMPERATURE
RANGE
MS-122
MIL.G-7711
MIL-C-21567
MIL-G-81322
MOBIL
GREASE
28
ROYCO
22
S
AEROSHELL
GREASE
22
SEE
NEXT
PAGE
FOR
SPECIAL
INSTRUCTIONS,
NOTES
AND
CAUTIONS.
Issued:
1/3/78
IC16
HANDLING
AND
SERVICING

Piper Lance II Specifications

General

Manufacturer	Piper Aircraft
Max Takeoff Weight	3, 600 lb (1, 633 kg)
Crew	1
Horsepower	300 hp
Seats	6
Length	27 ft 7 in (8.41 m)
Capacity	5 passengers